Airworthiness Directives; Bell Helicopter Textron, Inc. Model 205A, 205A-1, 205B, 212, 412, 412EP, and 412CF Helicopters
airworthiness · Rule · Final rule. · Published 2002-05-03 · Effective 2002-06-07 · 67 FR 22349
Document
Document number
02-10650
Federal Register citation
67 FR 22349
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2002-05-03
Effective date
2002-06-07
FAA docket
Docket No. 2001-SW-37-AD
Abstract
This amendment adopts a new airworthiness directive (AD) for Bell Helicopter Textron, Inc. (BHTI) Model 205A, 205A-1, 205B, 212, 412, 412EP, and 412CF helicopters, that requires inspecting each affected tail rotor blade forward tip weight retention block (tip block) and the aft tip closure (tip closure) for adhesive bond voids, and removing any tail rotor blade with an excessive void from service. This AD also requires modifying certain tail rotor blades by installing shear pins and tip closure rivets. This amendment is prompted by five occurrences of missing tip blocks or tip closures resulting in minor to substantial damage. The actions specified by this AD are intended to prevent loss of a tip block or tip closure, loss of a tail rotor blade, and subsequent loss of control of the helicopter.